What aerodynamic phenomenon most directly contributes to translational lift?

The aerodynamic phenomenon that most directly contributes to translational lift is the increased efficiency of the rotor system as the helicopter gains forward airspeed. When a helicopter is hovering, the rotor system induces a significant amount of downward airflow (induced flow) through the rotor disk. This induced flow reduces the effective angle of attack and requires the rotor blades to operate at a higher pitch angle to maintain lift, which increases drag and reduces efficiency. As the helicopter begins to move forward, the rotor system starts to operate in cleaner, undisturbed air. The induced flow becomes more horizontal, and the rotor blades work more efficiently, producing more lift for the same amount of power. This improved efficiency continues as airspeed increases until the helicopter reaches effective translational lift (ETL), usually around 16-24 knots. At ETL, the rotor system has completely outrun the recirculating air, and the induced flow is significantly reduced. This results in a substantial increase in lift and a decrease in vibration and noise. In essence, translational lift is a result of the rotor blades encountering a cleaner, less turbulent airflow as the helicopter moves forward, leading to greater aerodynamic efficiency and increased lift.